US8959717B2 - Circumferential strain rotary detent - Google Patents

Circumferential strain rotary detent Download PDF

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US8959717B2
US8959717B2 US13/796,570 US201313796570A US8959717B2 US 8959717 B2 US8959717 B2 US 8959717B2 US 201313796570 A US201313796570 A US 201313796570A US 8959717 B2 US8959717 B2 US 8959717B2
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Prior art keywords
hub
detent device
ridges
grooves
detent
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US20130237328A1 (en
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Philip A. Billings
George Larson
Timothy W. Jenum
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Reell Precision Manufacturing Corp
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Reell Precision Manufacturing Corp
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Assigned to REELL PRECISION MANUFACTURING CORPORATION reassignment REELL PRECISION MANUFACTURING CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BILLINGS, PHILIP A., JENUM, TIMOTHY W., LARSON, GEORGE
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Assigned to JPMORGAN CHASE BANK, N.A. reassignment JPMORGAN CHASE BANK, N.A. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: REELL PRECISION MANUFACTURING CORPORATION
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D7/00Slip couplings, e.g. slipping on overload, for absorbing shock
    • F16D7/002Slip couplings, e.g. slipping on overload, for absorbing shock the torque being transmitted and limited by yielding of an elastomeric race
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00Additional features or accessories of hinges
    • E05D11/10Devices for preventing movement between relatively-movable hinge parts
    • E05D11/1028Devices for preventing movement between relatively-movable hinge parts for maintaining the hinge in two or more positions, e.g. intermediate or fully open
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D11/00Additional features or accessories of hinges
    • E05D11/10Devices for preventing movement between relatively-movable hinge parts
    • E05D11/1028Devices for preventing movement between relatively-movable hinge parts for maintaining the hinge in two or more positions, e.g. intermediate or fully open
    • E05D2011/1035Devices for preventing movement between relatively-movable hinge parts for maintaining the hinge in two or more positions, e.g. intermediate or fully open with circumferential and evenly distributed detents around the pivot-axis

Definitions

  • Detent features are used in commercial products to establish a user experience indicating a home, closed or operating position.
  • a detent feature and a complementary second detent feature mating with the first detent feature are used to define a type of camming action during their relative movement.
  • Such features do so by providing a holding force in a home position, assuring the user that the device is being used in a proper position.
  • Such features may also provide a “self-closing” force to help the user achieve a home position.
  • Such detent devices may additionally provide protection to the device during exposure to abuse conditions such as transportation shock and vibration.
  • FIG. 1 illustrates an exploded perspective view of a detent device in accordance with one embodiment.
  • FIG. 2 illustrates a cross-sectional view of a detent device in accordance with one embodiment.
  • FIGS. 3 a - 3 b illustrate cross-sectional views of a rotated detent device in accordance with one embodiment.
  • FIG. 3 c illustrates a torque versus angle relationship for the detent device in accordance with FIGS. 3 a - 3 b.
  • FIG. 4 illustrates an exploded perspective view of a detent device in accordance with one embodiment.
  • FIGS. 5 a - 5 d illustrate partial views of a detent device in accordance with FIG. 4 , and illustrate alternate complementary geometries.
  • FIGS. 6 a - 6 b illustrate exploded perspective views of detent devices in accordance with alternative embodiments.
  • FIG. 7 illustrates a detent device implemented in a hinge design in accordance with one embodiment.
  • FIG. 8 illustrates a detent device implemented in a hinge design in accordance with one embodiment.
  • FIG. 1 illustrates detent device 10 in accordance with one embodiment.
  • Detent device 10 includes first hub 20 and second hub 30 .
  • first and second hubs 20 and 30 are generally cylindrical and first hub 20 is configured to be inserted within second hub 30 .
  • First hub 20 includes first through fourth protruding ridges 21 , 22 , 23 , and 24 (ridges 23 and 24 are not visible in FIG. 1 , but illustrated in FIG. 2 ) on its outer periphery and second hub 30 includes first through fourth receiving grooves 31 , 32 , 33 , 34 on its inner periphery.
  • first through fourth protruding ridges 21 , 22 , 23 , and 24 are configured to mate with first through fourth receiving grooves 31 , 32 , 33 , 34 .
  • first and second hubs 20 and 30 are configured to rotate relative to each other with first hub 20 within second hub 30 .
  • the relative rotation produces variable torque characteristics that are favorable for many applications.
  • first through fourth protruding ridges 21 - 24 are mated with first through fourth receiving grooves 31 - 34 , that is, when detent device 10 is in a “home position,” a first force is require to rotate first hub 20 relative to second hub 30 .
  • ridges 21 - 24 move out of grooves 31 - 34 , a second force higher than the first force is required for relative rotation of first hub 20 within second hub 30 .
  • a third force lower than the second force, but higher than the first force, is required for relative rotation of first hub 20 within second hub 30 .
  • a fourth force lower than each of first, second and third forces is required for relative rotation of first hub 20 within second hub 30 .
  • fourth force is a relative negative force such that first hub 20 tends to rotate relative to second hub 30 under the influence of the fourth force.
  • second hub 30 is made of engineering plastic that will allow the needed circumferential expansion second hub 30 as ridges 21 - 24 push against second hub 30 as they rotate out of corresponding grooves 31 - 34 .
  • the engineering plastic also offers good wear properties for detent device 10 , such that there is no need for lubricant between first and second hubs 20 and 30 .
  • detent device can withstand many thousands of cycles of relative rotation of first hub 20 relative to second hub 30 without significant variations in the applicable forces (first through fourth referred to above) and without lubricant.
  • First hub 20 can be made of either metal or engineering plastic that has good wear properties when in normal contact with second hub 30 .
  • FIG. 2 is a cross-sectional view of detent device 10 in accordance with one embodiment.
  • first through fourth protruding ridges 21 - 24 are mated or aligned with first through fourth receiving grooves 31 - 34 such that detent device 10 is in the home position.
  • FIG. 3 a illustrates detent device 10 with first hub 20 rotated 45 degrees relative to second hub 30 .
  • first ridge 21 is 45 degrees advanced in a clockwise direction relative to first groove 31
  • second ridge 22 is 45 degrees advanced in a clockwise direction relative to second groove 32
  • third ridge 23 is 45 degrees advanced in a clockwise direction relative to third groove 33
  • fourth ridge 24 is 45 degrees advanced in a clockwise direction relative to fourth groove 34 .
  • second hub 30 both expands circumferentially—creating hoop strain energy—and bends out-of-round between the contacting ridges 21 - 24 of first hub 20 , creating bending strain energy.
  • detent device 10 is configured such that the rotation of first hub 20 and resultant out-of-round bending of second hub 30 causes inner surface 35 of second hub 30 to actually contact outer surface 25 of first hub 20 .
  • Configuring detent device 10 in this manner actually limits the amount of bending strain in second hub 30 , and increases the amount of circumferential strain.
  • an optimal amount of bending versus circumferential strain may be achieved, creating very efficient energy storage in the detent device without exceeding stress design limits.
  • inner surface 35 of second hub 30 is illustrated as circular in its home position in FIG.
  • first hub 20 (apart from the receiving grooves 31 - 34 ), it may be other than circular in shape to achieve the desired optimization of bending and circumferential strain.
  • non-ridge portions of outer surface 25 of first hub 20 could also be other than circular in the home position in alternative embodiments.
  • detent device 10 is configured with relative circumferences for inner surface 35 and outer surface 25 and relative heights for protruding ridges 21 - 24 such that the effective circumferential strain in second hub 30 causes at least 2% strain on the material of second hub 30 .
  • the material is engineered plastic.
  • the material of second hub 30 is acetal or nylon. If the material of second hub 30 were a metal, such as hardened steel, a 2% strain on the material would cause the second hub 30 to break after upon repeated cycles of relative rotation of the hubs. Because second hub 30 is engineered plastic, however, this amount of strain provides favorable force characteristics of detent device 10 over many thousands of cycles between the hubs.
  • Outer surface 25 defines an effective diameter for first hub 20 .
  • the height of each of protruding ridges 21 - 24 extending in the radial direction from surface 25 does not exceed 4% of the effective diameter of first hub 20 . This relationship of ridge height to hub diameter also controls the amount of strain on the hub and contributes to the favorable force characteristics of detent device 10 over many thousands of cycles between the hubs.
  • FIG. 3 b also illustrates first hub 20 rotated 45 degrees relative to second hub 30 .
  • four positional lines are illustrated extending from the center of detent device 30 through discrete positions around the circumference of the device: a first line A intersect approximately the center of first groove 31 ; a second line B intersects approximately an edge of groove 31 (the edge that is on a side closer to groove 32 ); a third line C intersect approximately a midpoint between grooves 31 and 32 ; and a fourth line D intersects approximately an edge of groove 32 (the edge that is on a side closer to groove 31 ).
  • the first line A is repeated intersecting approximately the center of groove 32 illustrating the cyclic nature of detent device 10 .
  • These lines A-D illustrate relative rotational relationships of first and second hubs 20 and 30 throughout 90 degrees, which are then used to illustrate the corresponding force relationships.
  • FIG. 3 c illustrates the force or torque required to move first hub 20 relative to second hub 30 throughout 90 degrees. Using the four positions illustrated in FIG. 3 b , FIG. 3 c illustrates the required force at each of these approximate positions.
  • Position A that is, the position where each of ridges 21 - 24 are mated with each of grooves 31 - 34 (illustrated in FIG. 2 ) represents the home position. There is generally a holding force in this position that is dependent on the amount of interference between ridges 21 - 24 of first hub 20 with grooves 31 - 34 of second hub 30 . Moving from this home position generally requires some force, a first force represented generally at the position labeled A on FIG. 3 c , because this force holds the device in this position.
  • Position B that is, the position where each of ridges 21 - 24 are moving out of each of grooves 31 - 34 represents the initial transition position.
  • the initial transition position represents the movement of first hub 20 out of its home position up to a point of maximum interference with the inner surface 35 of second hub 30 .
  • this represents the maximum force condition, a second force represented generally at the position labeled B on FIG. 3 c , for detent device 10 .
  • This maximum force is largely governed by the respective dimensions and interference of the ridges 21 - 24 and grooves 31 - 34 .
  • Position C that is, the position where first hub 20 rotated 45 degrees relative to second hub 30 (as illustrated in FIG. 3 b ) represents the frictional position.
  • the frictional position is a condition where most of the force, a third force represented generally at the position labeled C on FIG. 3 c , to maintain movement of first hub 20 relative to second hub 30 is frictional, caused by the interference of the protruding ridges 21 - 24 of first hub 20 with the inner surface 35 of second hub 30 .
  • Position D that is, the position where ridges 21 - 24 of first hub 20 are re-entering receiving grooves 31 - 34 of second hub 30 .
  • this fourth force represented generally at the position labeled D on FIG. 3 c , may actually be negative before the home position is reached, causing first hub 20 to “self-rotate” unless a restraining (negative) force is applied to prevent such motion.
  • detent device 10 provides a force versus angle relationship that is useful in a variety of applications. Furthermore, configuring the circumference of outer surface 25 of first hub 20 relative to the circumference of inner surface 35 of second hub 30 provides control of both circumferential strain and bending strain of second hub 30 . This provides favorable spring function in detent device 10 allowing an efficient device requiring a relatively small space. Configuring second hub 35 of an engineered plastic further allows a detent device 10 that is free of any kind of lubrication. This simplifies the design, yet provides thousands of cycles of relative rotation of first and second hubs 20 and 30 while maintaining a substantially consistent force versus angle relationship over these thousands of cycles.
  • FIG. 4 illustrates detent device 50 in accordance with one embodiment.
  • Detent device 50 includes first hub 60 and second hub 70 , and in one embodiment, first and second hubs 60 and 70 are generally cylindrical with first hub 60 configured to be inserted within second hub 70 .
  • First hub 60 includes first through fourth receiving grooves 61 , 62 , 63 , and 64 (grooves 63 and 64 are not visible in FIG. 4 ) on its outer surface 65 and second hub 70 includes first through fourth protruding ridges 71 , 72 , 73 , and 74 on its inner surface 75 .
  • first through fourth receiving grooves 61 , 62 , 63 , and 64 are configured to mate with first through fourth protruding ridges 71 , 72 , 73 , and 74 .
  • Detent device 50 operates similarly to detent device 10 as described above, but with protruding ridges 71 , 72 , 73 , and 74 and receiving grooves 61 , 62 , 63 , and 64 reversed relative to inner surface 75 of second hub 70 and outer surface 65 of first hub 60 .
  • Second hub 70 must still allow for circumferential expansion, so its preferred material is a wear resistant engineering plastic, such as acetal or nylon.
  • the circumference of outer surface 65 of first hub 60 is still configured relative to the circumference of inner surface 75 of second hub 70 to control and limit both circumferential strain and bending strain of second hub 70 to provide favorable spring function in a relatively small space.
  • first hubs 20 / 60 and second hubs 30 / 70 retains the essential detent function from circumferential tensile strain of second hub 70 ( FIG. 4 )
  • first hubs 20 / 60 of a more compliant material than second hub 30 / 70 will result in circumferential compressive strain of first hub 20 / 60 , achieving the same detent function.
  • outer surface 25 / 65 of first hub 20 / 60 and inner surface 35 / 75 of second hub 30 / 70 are illustrated as having complementary mating geometries.
  • complementary mating geometries of the two detent surfaces—protruding ridges 21 / 71 , 22 / 72 , 23 / 73 , and 24 / 74 and receiving grooves 31 / 61 , 32 / 62 , 33 / 63 , and 34 / 64 in the illustrated embodiments—it is meant that the surfaces are functionally complementary, and that one feature moves radially inward towards the other when the two features are aligned (home position), allowing second hub 30 / 70 to relax its circumferential expansion and lower the normal force between the two features.
  • a protruding ridge moves at least partway into a receiving groove (or the opposite, depending on which hub has which feature).
  • FIGS. 5 a - 5 d illustrate embodiments of various complementary mating geometries for first ridge 71 and first grove 61 from detent device 50 .
  • FIG. 5 a illustrates first ridge 71 a and first grove 61 a with geometries that are substantially dimensionally equivalent, such that when it the home position first ridge 71 and first grove 61 share an adjacent border.
  • FIGS. 5 b - 5 d illustrate alternate complementary mating geometries for first ridge 71 b/c/d and first grove 61 b/c/d that are not dimensionally equivalent, but that achieve the same functional result.
  • cam design will understand that normal design methodologies are used to determine the profiles of the protruding ridges and receiving grooves in a manner that results in desirable and allowable forces, energy storage, contact stresses, and wear.
  • Detent devices 10 and 50 are illustrated with four protruding ridges and four receiving grooves spaced substantially equidistant around the respective perimeters of the hubs.
  • Other embodiments can use less protrusions and complementary grooves, for example one, two or three.
  • larger numbers of protrusions and complementary grooves can be used.
  • the spacing between the pairs of protrusions and complementary grooves can be varied around the circumference of the hubs dependent on the desired performance characteristics of the detent device.
  • FIG. 6 a illustrates detent device 90 in accordance with one embodiment.
  • Detent device 90 includes first hub 100 and second hub 110 .
  • First hub 100 includes first hub main portion 106 and first hub connection portion 108 and second hub 110 includes second hub main portion 116 and second hub connection portion 118 .
  • first and second hub main portions 106 and 116 are generally cylindrical with first hub main portion 106 configured to be inserted within second hub main portion 116 , thereby providing a detent device with operational characteristics consistent with that described above with respect to devices 10 and 50 .
  • First hub main portion 106 includes first through fourth protruding ridges 101 , 102 , 103 , and 104 (ridges 103 and 104 are not visible in FIG. 6 a ) on its outer surface and second hub main portion 116 includes first through fourth receiving grooves 111 , 112 , 113 , and 114 on its inner surface.
  • first through fourth receiving grooves 111 , 112 , 113 , and 114 are configured to mate with first through fourth protruding ridges 101 , 102 , 103 , and 104 .
  • first and second hub connection portions 108 and 118 facilitate the circumferential expansion of first and second hubs 100 and 110 and allow connection of detent device 90 into further mechanism, such as hinges.
  • First and second hub connection portions 108 and 118 can be readily coupled to other devices, such as hinge devices, for controlled relative rotations providing force versus angle characteristics similar to that illustrated in FIG. 3 c due to the interaction of first hub main portion 106 and second hub main portion 116 .
  • FIG. 6 b illustrates detent device 130 in accordance with one embodiment.
  • Detent device 130 includes first hub 140 and second hub 150 .
  • First hub 140 includes first hub main portion 146 and first hub connection portion 148 and second hub 150 includes second hub main portion 166 and second hub connection portion 168 .
  • first and second hub main portions 146 and 166 are generally cylindrical with first hub main portion 146 configured to be inserted within second hub main portion 166 , thereby providing a detent device with operational characteristics consistent with that described above with respect to devices 10 and 50 .
  • First hub main portion 146 includes first through fourth protruding ridges 141 , 142 , 143 , and 144 on its outer surface and second hub main portion 166 includes first through fourth receiving grooves 151 , 152 , 153 , and 154 on its inner surface.
  • first through fourth receiving grooves 141 , 142 , 143 , and 144 are configured to mate with first through fourth protruding ridges 151 , 152 , 153 , and 154 .
  • first and second hub connection portions 148 and 168 facilitate the radial expansion of first and second hubs 140 and 150 and allow connection of detent device 130 into further mechanism, such as hinges.
  • First hub main portion 146 is expanded axially relative to second hub main portion 166 , such that once first hub main portion 146 is inserted into second hub main portion 166 , a section of first hub main portion 146 that is coupled to first hub connection portion 148 extends outside second hub main portion 166 such that there is no interference between second hub main portion 166 and first hub connection portion 148 .
  • first and second hub connection portions 148 and 168 can be readily coupled to other devices, such as hinge devices, for controlled relative rotations.
  • Embodiments such as illustrated for detent devices 10 , 50 , 90 and 130 , provide controlled relative rotation having force versus angle characteristics similar to that illustrated in FIG. 3 c .
  • These detent devices are light weight with utilization of engineering plastics for the hubs. Furthermore, these devices are lubricant free, yet able to provide repeatable torque over many thousands of cycles of relative rotation of the hubs.
  • the devices are spatially efficient through the storage of energy by circumferential as well as bending strain.
  • the detent devices are easy to assemble and contain a minimum number of parts.
  • FIG. 7 illustrates a partially exploded view of detent hinge 170 in accordance with one embodiment.
  • detent hinge 170 illustrates a practical implementation of two detent devices, such as detent device 10 described above.
  • Detent hinge 170 includes first, second, and third hinge sections 180 , 190 and 200 .
  • First hinge section 180 includes first connection 184 and first receiving hub 182 .
  • Second hinge section 190 includes second connection 196 , first extending hub 194 , and second extending hub 192 .
  • Third hinge section 200 includes third connection 204 and second receiving hub 202 .
  • first extending hub 194 of second hinge section 190 is inserted in first receiving hub 182 of first hinge section 180 .
  • first extending hub 194 includes a plurality of ridges and first receiving hub 182 includes a plurality of receiving grooves configured to mate with the ridges, similar to that described above with the various detent devices.
  • second extending hub 192 of second hinge section 190 is inserted in second receiving hub 202 of third hinge section 200 .
  • second extending hub 192 includes a plurality of ridges and second receiving hub 202 includes a plurality of receiving grooves configured to mate with the ridges, similar to that described above with the various detent devices.
  • first and second receiving hubs 182 and 202 are configured to circumferentially expand, thereby providing both circumferential and bending strain.
  • first, second, and third hinge sections 180 , 190 and 200 are coupled to two or more bodies for relative rotation.
  • second connection 196 can be mounted to a base of a laptop computer
  • first connection 184 and third connection 204 are coupled to a screen of the laptop computer. This allows the screen of the computer to rotate relative to the base under the force influence of the two detent devices formed from the combination of first receiving hub 182 of first hinge section 180 rotating about first extending hub 194 of second hinge section 190 and second receiving hub 202 of third hinge section 200 rotating about second extending hub 192 of second hinge section 190 .
  • the torque profile in one embodiment is similar to that given in FIG. 3 c.
  • first, second, and third hinge sections 180 , 190 and 200 can be mounted to three different rotatable bodies.
  • second connection 196 can be mounted to a base, while first and third hinge sections 180 and 200 are respectively each mounted to first and second rotatable bodies.
  • the first body is rotatable relative to the base under the influence of the detent device formed from first receiving hub 182 of first hinge section 180 rotating about first extending hub 194 of second hinge section 190 .
  • the second body is rotatable relative to the base under the influence of the detent device formed from second receiving hub 202 of third hinge section 200 rotating about second extending hub 192 of second hinge section 190 .
  • FIG. 8 illustrates detent friction hinge 210 in accordance with one embodiment.
  • Detent friction hinge combines a detent device, such as described above with respect to detent devices 10 and 50 , with a friction hinge, that is, a constant torque clutch, in order to achieve a higher and more controlled friction between detent positions.
  • detent friction hinge 210 includes first hinge portion 212 , second hinge portion 218 , first hub 214 and second hub 216 .
  • First hinge portion 212 is mounted to a first hinged body and second hinge portion 218 is mounted to a second hinged body, such that the first and second hinges bodies can be rotated relative to each other under the control of detent friction hinge 210 .
  • a plurality of frictional elements 220 are provided between first hinge portion 212 and second hinge portion 218 to provide a frictional rotational force therebetween (in FIG. 8 , a portion of second hinge portion 218 is cut away to partially reveal frictional elements 220 ).
  • first hub 214 in configured with protruding ridges and second hub 216 is configured with grooves to form complementary mating geometries.
  • detent friction hinge 210 creates resistance to rotation from frictional elements 220 between first hinge portion 212 and second hinge portion 218 , as well as from the resistance of the protruding ridges of first hub 214 with the receiving grooves of second hub 216 .
  • Frictional elements 220 essentially work in series with the detent device created by first and second hubs 214 and 216 .
  • detent friction hinge 210 accordingly provides controlled friction between detent positions, while providing a user with a sense of reaching a desired home position, a reduction of force during this final movement, and a firm holding force once in the home position.

Abstract

One aspect is a detent device with a first hub having an axis and comprising a first feature having both a radial and an axial dimension relative to the hub axis, and having a first hub connection portion. A second hub is located co-axially outside the first hub and comprises a second feature having both a radial and an axial dimension relative to the hub axis, the second feature of the second hub touching the first feature of the first hub when the features are aligned. The second hub has a second hub connection portion. The first and second features have complementary mating geometries. The detent device is configured such that when relative movement is provided to the first and second hub connection portions, a circumferential strain energy of the second hub changes, providing a variable force between the two connection portions depending on their relative position.

Description

CROSS REFERENCE TO RELATED APPLICATIONS
This Non-Provisional Patent Application claims the benefit of the filing date of U.S. Provisional Patent Application Ser. No. 61/609,604, filed Mar. 12, 2012, entitled “CIRCUMFERENTIAL STRAIN ROTARY DETENT”, which is herein incorporated by reference.
BACKGROUND
Detent features are used in commercial products to establish a user experience indicating a home, closed or operating position. Typically, a detent feature and a complementary second detent feature mating with the first detent feature are used to define a type of camming action during their relative movement. Such features do so by providing a holding force in a home position, assuring the user that the device is being used in a proper position. Such features may also provide a “self-closing” force to help the user achieve a home position. Such detent devices may additionally provide protection to the device during exposure to abuse conditions such as transportation shock and vibration.
Historically, numerous types of loading means have been used between two detent features, among them leaf springs, torsion springs, and compression springs. Often the spring may also serve as one of the two detent features in frictional contact with the other feature. The means of spring loading the first detent feature to the second detent feature allows for both energy storage as well as normal and tangential force loading between the two features. This energy storage and force varies as the device is moved out of one detent position to the next detent position.
However, these loading devices suffer the drawback of storing energy principally through only one type of deflection: torsional strain (compression springs), or bending strain (torsion springs and leaf springs). As a result, these devices must often be large and bulky to achieve the required energy storage and force required. Reducing the size of these devices while maintaining or increasing the energy and force requirements often results in either excessive stresses which may fatigue and/or break the spring element, or excessive frictional wear between the two detent features which degrades performance and the user experience.
Many of the current technologies utilize hardened steel to achieve smaller size while accommodating higher stresses and forces, but do so by requiring an oil or grease to lubricate the complementary detent components to avoid galling.
Many technologies also require more complex assembly methods and a higher number of components. Additionally, other technologies requiring metallic components to ensure reasonable wear and component stresses will have a higher weight, a drawback if weight sensitive components are required, for example, in aircraft.
For these and other reasons, a need exists for the present invention.
BRIEF DESCRIPTION OF THE DRAWINGS
The accompanying drawings are included to provide a further understanding of embodiments and are incorporated in and constitute a part of this specification. The drawings illustrate embodiments and together with the description serve to explain principles of embodiments. Other embodiments and many of the intended advantages of embodiments will be readily appreciated as they become better understood by reference to the following detailed description. The elements of the drawings are not necessarily to scale relative to each other. Like reference numerals designate corresponding similar parts.
FIG. 1 illustrates an exploded perspective view of a detent device in accordance with one embodiment.
FIG. 2 illustrates a cross-sectional view of a detent device in accordance with one embodiment.
FIGS. 3 a-3 b illustrate cross-sectional views of a rotated detent device in accordance with one embodiment.
FIG. 3 c illustrates a torque versus angle relationship for the detent device in accordance with FIGS. 3 a-3 b.
FIG. 4 illustrates an exploded perspective view of a detent device in accordance with one embodiment.
FIGS. 5 a-5 d illustrate partial views of a detent device in accordance with FIG. 4, and illustrate alternate complementary geometries.
FIGS. 6 a-6 b illustrate exploded perspective views of detent devices in accordance with alternative embodiments.
FIG. 7 illustrates a detent device implemented in a hinge design in accordance with one embodiment.
FIG. 8 illustrates a detent device implemented in a hinge design in accordance with one embodiment.
DETAILED DESCRIPTION
In the following Detailed Description, reference is made to the accompanying drawings, which form a part hereof, and in which is shown by way of illustration specific embodiments in which the invention may be practiced. In this regard, directional terminology, such as “top,” “bottom,” “front,” “back,” “leading,” “trailing,” etc., is used with reference to the orientation of the Figure(s) being described. Because components of embodiments can be positioned in a number of different orientations, the directional terminology is used for purposes of illustration and is in no way limiting. It is to be understood that other embodiments may be utilized and structural or logical changes may be made without departing from the scope of the present invention. The following detailed description, therefore, is not to be taken in a limiting sense, and the scope of the present invention is defined by the appended claims.
It is to be understood that the features of the various exemplary embodiments described herein may be combined with each other, unless specifically noted otherwise.
FIG. 1 illustrates detent device 10 in accordance with one embodiment. Detent device 10 includes first hub 20 and second hub 30. In one embodiment, first and second hubs 20 and 30 are generally cylindrical and first hub 20 is configured to be inserted within second hub 30. First hub 20 includes first through fourth protruding ridges 21, 22, 23, and 24 ( ridges 23 and 24 are not visible in FIG. 1, but illustrated in FIG. 2) on its outer periphery and second hub 30 includes first through fourth receiving grooves 31, 32, 33, 34 on its inner periphery. In one embodiment, first through fourth protruding ridges 21, 22, 23, and 24 are configured to mate with first through fourth receiving grooves 31, 32, 33, 34.
In one embodiment, first and second hubs 20 and 30 are configured to rotate relative to each other with first hub 20 within second hub 30. The relative rotation produces variable torque characteristics that are favorable for many applications. When first through fourth protruding ridges 21-24 are mated with first through fourth receiving grooves 31-34, that is, when detent device 10 is in a “home position,” a first force is require to rotate first hub 20 relative to second hub 30. As ridges 21-24 move out of grooves 31-34, a second force higher than the first force is required for relative rotation of first hub 20 within second hub 30. Once ridges 21-24 move away from grooves 31-34, a third force, lower than the second force, but higher than the first force, is required for relative rotation of first hub 20 within second hub 30. As ridges 21-24 then begin to move back into grooves 31-34, a fourth force lower than each of first, second and third forces, is required for relative rotation of first hub 20 within second hub 30. In one embodiment, fourth force is a relative negative force such that first hub 20 tends to rotate relative to second hub 30 under the influence of the fourth force.
In one embodiment, second hub 30 is made of engineering plastic that will allow the needed circumferential expansion second hub 30 as ridges 21-24 push against second hub 30 as they rotate out of corresponding grooves 31-34. At the same time, the engineering plastic also offers good wear properties for detent device 10, such that there is no need for lubricant between first and second hubs 20 and 30. As such, detent device can withstand many thousands of cycles of relative rotation of first hub 20 relative to second hub 30 without significant variations in the applicable forces (first through fourth referred to above) and without lubricant. First hub 20 can be made of either metal or engineering plastic that has good wear properties when in normal contact with second hub 30.
FIG. 2 is a cross-sectional view of detent device 10 in accordance with one embodiment. In FIG. 2, first through fourth protruding ridges 21-24 are mated or aligned with first through fourth receiving grooves 31-34 such that detent device 10 is in the home position. In one embodiment, there is a slight interference of protruding ridges 21-24 with each of the respective receiving grooves in second hub 30 in order to ensure an adequate holding force in the home position. Clearance is provided between nominal first hub outer surface 25 and nominal second hub inner surface 35 in order to optimize the transition force as first hub 20 rotates relative to second hub 30.
FIG. 3 a illustrates detent device 10 with first hub 20 rotated 45 degrees relative to second hub 30. As such, first ridge 21 is 45 degrees advanced in a clockwise direction relative to first groove 31, second ridge 22 is 45 degrees advanced in a clockwise direction relative to second groove 32, third ridge 23 is 45 degrees advanced in a clockwise direction relative to third groove 33, and fourth ridge 24 is 45 degrees advanced in a clockwise direction relative to fourth groove 34. As the protruding ridges 21-24 of first hub 20 are forced out of the corresponding receiving grooves 31-34 of second hub 30, second hub 30 both expands circumferentially—creating hoop strain energy—and bends out-of-round between the contacting ridges 21-24 of first hub 20, creating bending strain energy.
These two elastic strains, circumferential strain and bending strain, serve as a spring function in detent device 10. The combination of circumferential and bending strain creates an efficient detent mechanism requiring a smaller space than those relying principally on one kind of strain energy. The interference of the protruding ridges 21-24 with the inner surface 35 of second hub 30 will determine the frictional force to continue rotating first hub 20 relative to second hub 30 in the condition illustrated in FIG. 3 a.
In one embodiment, detent device 10 is configured such that the rotation of first hub 20 and resultant out-of-round bending of second hub 30 causes inner surface 35 of second hub 30 to actually contact outer surface 25 of first hub 20. Configuring detent device 10 in this manner actually limits the amount of bending strain in second hub 30, and increases the amount of circumferential strain. By appropriately configuring the physical dimensions of the device, an optimal amount of bending versus circumferential strain may be achieved, creating very efficient energy storage in the detent device without exceeding stress design limits. One skilled in the art will also appreciate that, although inner surface 35 of second hub 30 is illustrated as circular in its home position in FIG. 2 (apart from the receiving grooves 31-34), it may be other than circular in shape to achieve the desired optimization of bending and circumferential strain. Similarly, although illustrated as circular, the non-ridge portions of outer surface 25 of first hub 20 could also be other than circular in the home position in alternative embodiments.
In one embodiment, detent device 10 is configured with relative circumferences for inner surface 35 and outer surface 25 and relative heights for protruding ridges 21-24 such that the effective circumferential strain in second hub 30 causes at least 2% strain on the material of second hub 30. In one embodiment, the material is engineered plastic. In various embodiments, the material of second hub 30 is acetal or nylon. If the material of second hub 30 were a metal, such as hardened steel, a 2% strain on the material would cause the second hub 30 to break after upon repeated cycles of relative rotation of the hubs. Because second hub 30 is engineered plastic, however, this amount of strain provides favorable force characteristics of detent device 10 over many thousands of cycles between the hubs.
Outer surface 25 defines an effective diameter for first hub 20. In one embodiment, the height of each of protruding ridges 21-24 extending in the radial direction from surface 25 does not exceed 4% of the effective diameter of first hub 20. This relationship of ridge height to hub diameter also controls the amount of strain on the hub and contributes to the favorable force characteristics of detent device 10 over many thousands of cycles between the hubs.
FIG. 3 b also illustrates first hub 20 rotated 45 degrees relative to second hub 30. In addition, four positional lines are illustrated extending from the center of detent device 30 through discrete positions around the circumference of the device: a first line A intersect approximately the center of first groove 31; a second line B intersects approximately an edge of groove 31 (the edge that is on a side closer to groove 32); a third line C intersect approximately a midpoint between grooves 31 and 32; and a fourth line D intersects approximately an edge of groove 32 (the edge that is on a side closer to groove 31). The first line A is repeated intersecting approximately the center of groove 32 illustrating the cyclic nature of detent device 10. These lines A-D illustrate relative rotational relationships of first and second hubs 20 and 30 throughout 90 degrees, which are then used to illustrate the corresponding force relationships.
FIG. 3 c illustrates the force or torque required to move first hub 20 relative to second hub 30 throughout 90 degrees. Using the four positions illustrated in FIG. 3 b, FIG. 3 c illustrates the required force at each of these approximate positions.
Position A, that is, the position where each of ridges 21-24 are mated with each of grooves 31-34 (illustrated in FIG. 2) represents the home position. There is generally a holding force in this position that is dependent on the amount of interference between ridges 21-24 of first hub 20 with grooves 31-34 of second hub 30. Moving from this home position generally requires some force, a first force represented generally at the position labeled A on FIG. 3 c, because this force holds the device in this position.
Position B, that is, the position where each of ridges 21-24 are moving out of each of grooves 31-34 represents the initial transition position. The initial transition position represents the movement of first hub 20 out of its home position up to a point of maximum interference with the inner surface 35 of second hub 30. In one embodiment this represents the maximum force condition, a second force represented generally at the position labeled B on FIG. 3 c, for detent device 10. This maximum force is largely governed by the respective dimensions and interference of the ridges 21-24 and grooves 31-34.
Position C, that is, the position where first hub 20 rotated 45 degrees relative to second hub 30 (as illustrated in FIG. 3 b) represents the frictional position. The frictional position is a condition where most of the force, a third force represented generally at the position labeled C on FIG. 3 c, to maintain movement of first hub 20 relative to second hub 30 is frictional, caused by the interference of the protruding ridges 21-24 of first hub 20 with the inner surface 35 of second hub 30.
Position D, that is, the position where ridges 21-24 of first hub 20 are re-entering receiving grooves 31-34 of second hub 30. Depending on the dimensions of ridges 21-24 and protrusions 31-34, this fourth force, represented generally at the position labeled D on FIG. 3 c, may actually be negative before the home position is reached, causing first hub 20 to “self-rotate” unless a restraining (negative) force is applied to prevent such motion.
In one embodiment, detent device 10 provides a force versus angle relationship that is useful in a variety of applications. Furthermore, configuring the circumference of outer surface 25 of first hub 20 relative to the circumference of inner surface 35 of second hub 30 provides control of both circumferential strain and bending strain of second hub 30. This provides favorable spring function in detent device 10 allowing an efficient device requiring a relatively small space. Configuring second hub 35 of an engineered plastic further allows a detent device 10 that is free of any kind of lubrication. This simplifies the design, yet provides thousands of cycles of relative rotation of first and second hubs 20 and 30 while maintaining a substantially consistent force versus angle relationship over these thousands of cycles.
FIG. 4 illustrates detent device 50 in accordance with one embodiment. Detent device 50 includes first hub 60 and second hub 70, and in one embodiment, first and second hubs 60 and 70 are generally cylindrical with first hub 60 configured to be inserted within second hub 70. First hub 60 includes first through fourth receiving grooves 61, 62, 63, and 64 (grooves 63 and 64 are not visible in FIG. 4) on its outer surface 65 and second hub 70 includes first through fourth protruding ridges 71, 72, 73, and 74 on its inner surface 75. In one embodiment, first through fourth receiving grooves 61, 62, 63, and 64 are configured to mate with first through fourth protruding ridges 71, 72, 73, and 74.
Detent device 50 operates similarly to detent device 10 as described above, but with protruding ridges 71, 72, 73, and 74 and receiving grooves 61, 62, 63, and 64 reversed relative to inner surface 75 of second hub 70 and outer surface 65 of first hub 60. Second hub 70 must still allow for circumferential expansion, so its preferred material is a wear resistant engineering plastic, such as acetal or nylon. Also, the circumference of outer surface 65 of first hub 60 is still configured relative to the circumference of inner surface 75 of second hub 70 to control and limit both circumferential strain and bending strain of second hub 70 to provide favorable spring function in a relatively small space.
Just as reversing the ridges and grooves between first hubs 20/60 and second hubs 30/70 retains the essential detent function from circumferential tensile strain of second hub 70 (FIG. 4), one skilled in the art will understand that configuring first hubs 20/60 of a more compliant material than second hub 30/70 will result in circumferential compressive strain of first hub 20/60, achieving the same detent function.
In both detent devices 10 and 50, outer surface 25/65 of first hub 20/60 and inner surface 35/75 of second hub 30/70 are illustrated as having complementary mating geometries. By “complementary mating geometries” of the two detent surfaces—protruding ridges 21/71, 22/72, 23/73, and 24/74 and receiving grooves 31/61, 32/62, 33/63, and 34/64 in the illustrated embodiments—it is meant that the surfaces are functionally complementary, and that one feature moves radially inward towards the other when the two features are aligned (home position), allowing second hub 30/70 to relax its circumferential expansion and lower the normal force between the two features. In other words, a protruding ridge moves at least partway into a receiving groove (or the opposite, depending on which hub has which feature).
FIGS. 5 a-5 d illustrate embodiments of various complementary mating geometries for first ridge 71 and first grove 61 from detent device 50. FIG. 5 a illustrates first ridge 71 a and first grove 61 a with geometries that are substantially dimensionally equivalent, such that when it the home position first ridge 71 and first grove 61 share an adjacent border. FIGS. 5 b-5 d illustrate alternate complementary mating geometries for first ridge 71 b/c/d and first grove 61 b/c/d that are not dimensionally equivalent, but that achieve the same functional result. One skilled in the art of cam design will understand that normal design methodologies are used to determine the profiles of the protruding ridges and receiving grooves in a manner that results in desirable and allowable forces, energy storage, contact stresses, and wear.
Detent devices 10 and 50 are illustrated with four protruding ridges and four receiving grooves spaced substantially equidistant around the respective perimeters of the hubs. Other embodiments can use less protrusions and complementary grooves, for example one, two or three. Furthermore, larger numbers of protrusions and complementary grooves can be used. Also, the spacing between the pairs of protrusions and complementary grooves can be varied around the circumference of the hubs dependent on the desired performance characteristics of the detent device.
FIG. 6 a illustrates detent device 90 in accordance with one embodiment. Detent device 90 includes first hub 100 and second hub 110. First hub 100 includes first hub main portion 106 and first hub connection portion 108 and second hub 110 includes second hub main portion 116 and second hub connection portion 118. In one embodiment, first and second hub main portions 106 and 116 are generally cylindrical with first hub main portion 106 configured to be inserted within second hub main portion 116, thereby providing a detent device with operational characteristics consistent with that described above with respect to devices 10 and 50.
First hub main portion 106 includes first through fourth protruding ridges 101, 102, 103, and 104 (ridges 103 and 104 are not visible in FIG. 6 a) on its outer surface and second hub main portion 116 includes first through fourth receiving grooves 111, 112, 113, and 114 on its inner surface. In one embodiment, first through fourth receiving grooves 111, 112, 113, and 114 are configured to mate with first through fourth protruding ridges 101, 102, 103, and 104.
In one embodiment, first and second hub connection portions 108 and 118 facilitate the circumferential expansion of first and second hubs 100 and 110 and allow connection of detent device 90 into further mechanism, such as hinges. First and second hub connection portions 108 and 118 can be readily coupled to other devices, such as hinge devices, for controlled relative rotations providing force versus angle characteristics similar to that illustrated in FIG. 3 c due to the interaction of first hub main portion 106 and second hub main portion 116.
FIG. 6 b illustrates detent device 130 in accordance with one embodiment. Detent device 130 includes first hub 140 and second hub 150. First hub 140 includes first hub main portion 146 and first hub connection portion 148 and second hub 150 includes second hub main portion 166 and second hub connection portion 168. In one embodiment, first and second hub main portions 146 and 166 are generally cylindrical with first hub main portion 146 configured to be inserted within second hub main portion 166, thereby providing a detent device with operational characteristics consistent with that described above with respect to devices 10 and 50.
First hub main portion 146 includes first through fourth protruding ridges 141, 142, 143, and 144 on its outer surface and second hub main portion 166 includes first through fourth receiving grooves 151, 152, 153, and 154 on its inner surface. In one embodiment, first through fourth receiving grooves 141, 142, 143, and 144 are configured to mate with first through fourth protruding ridges 151, 152, 153, and 154.
In one embodiment, first and second hub connection portions 148 and 168 facilitate the radial expansion of first and second hubs 140 and 150 and allow connection of detent device 130 into further mechanism, such as hinges. First hub main portion 146 is expanded axially relative to second hub main portion 166, such that once first hub main portion 146 is inserted into second hub main portion 166, a section of first hub main portion 146 that is coupled to first hub connection portion 148 extends outside second hub main portion 166 such that there is no interference between second hub main portion 166 and first hub connection portion 148. In this way, first and second hub connection portions 148 and 168 can be readily coupled to other devices, such as hinge devices, for controlled relative rotations.
Embodiments, such as illustrated for detent devices 10, 50, 90 and 130, provide controlled relative rotation having force versus angle characteristics similar to that illustrated in FIG. 3 c. These detent devices are light weight with utilization of engineering plastics for the hubs. Furthermore, these devices are lubricant free, yet able to provide repeatable torque over many thousands of cycles of relative rotation of the hubs. The devices are spatially efficient through the storage of energy by circumferential as well as bending strain. The detent devices are easy to assemble and contain a minimum number of parts.
FIG. 7 illustrates a partially exploded view of detent hinge 170 in accordance with one embodiment. In one embodiment, detent hinge 170 illustrates a practical implementation of two detent devices, such as detent device 10 described above. Detent hinge 170 includes first, second, and third hinge sections 180, 190 and 200. First hinge section 180 includes first connection 184 and first receiving hub 182. Second hinge section 190 includes second connection 196, first extending hub 194, and second extending hub 192. Third hinge section 200 includes third connection 204 and second receiving hub 202.
When assembled, first extending hub 194 of second hinge section 190 is inserted in first receiving hub 182 of first hinge section 180. In one embodiment, first extending hub 194 includes a plurality of ridges and first receiving hub 182 includes a plurality of receiving grooves configured to mate with the ridges, similar to that described above with the various detent devices. Similarly, second extending hub 192 of second hinge section 190 is inserted in second receiving hub 202 of third hinge section 200. In one embodiment, second extending hub 192 includes a plurality of ridges and second receiving hub 202 includes a plurality of receiving grooves configured to mate with the ridges, similar to that described above with the various detent devices. Furthermore, first and second receiving hubs 182 and 202 are configured to circumferentially expand, thereby providing both circumferential and bending strain.
In operation, first, second, and third hinge sections 180, 190 and 200 are coupled to two or more bodies for relative rotation. For example, second connection 196 can be mounted to a base of a laptop computer, while first connection 184 and third connection 204 are coupled to a screen of the laptop computer. This allows the screen of the computer to rotate relative to the base under the force influence of the two detent devices formed from the combination of first receiving hub 182 of first hinge section 180 rotating about first extending hub 194 of second hinge section 190 and second receiving hub 202 of third hinge section 200 rotating about second extending hub 192 of second hinge section 190. The torque profile in one embodiment is similar to that given in FIG. 3 c.
In one embodiment, first, second, and third hinge sections 180, 190 and 200 can be mounted to three different rotatable bodies. For example, second connection 196 can be mounted to a base, while first and third hinge sections 180 and 200 are respectively each mounted to first and second rotatable bodies. As such, the first body is rotatable relative to the base under the influence of the detent device formed from first receiving hub 182 of first hinge section 180 rotating about first extending hub 194 of second hinge section 190. The second body is rotatable relative to the base under the influence of the detent device formed from second receiving hub 202 of third hinge section 200 rotating about second extending hub 192 of second hinge section 190.
FIG. 8 illustrates detent friction hinge 210 in accordance with one embodiment. Detent friction hinge combines a detent device, such as described above with respect to detent devices 10 and 50, with a friction hinge, that is, a constant torque clutch, in order to achieve a higher and more controlled friction between detent positions. In one embodiment, detent friction hinge 210 includes first hinge portion 212, second hinge portion 218, first hub 214 and second hub 216. First hinge portion 212 is mounted to a first hinged body and second hinge portion 218 is mounted to a second hinged body, such that the first and second hinges bodies can be rotated relative to each other under the control of detent friction hinge 210.
In one embodiment, a plurality of frictional elements 220 are provided between first hinge portion 212 and second hinge portion 218 to provide a frictional rotational force therebetween (in FIG. 8, a portion of second hinge portion 218 is cut away to partially reveal frictional elements 220). In addition, first hub 214 in configured with protruding ridges and second hub 216 is configured with grooves to form complementary mating geometries. As the first and second hinges bodies are rotated relative to each other, detent friction hinge 210 creates resistance to rotation from frictional elements 220 between first hinge portion 212 and second hinge portion 218, as well as from the resistance of the protruding ridges of first hub 214 with the receiving grooves of second hub 216. Frictional elements 220 essentially work in series with the detent device created by first and second hubs 214 and 216.
In one embodiment, detent friction hinge 210 accordingly provides controlled friction between detent positions, while providing a user with a sense of reaching a desired home position, a reduction of force during this final movement, and a firm holding force once in the home position.
Although specific embodiments have been illustrated and described herein, it will be appreciated by those of ordinary skill in the art that a variety of alternate and/or equivalent implementations may be substituted for the specific embodiments shown and described without departing from the scope of the present invention. This application is intended to cover any adaptations or variations of the specific embodiments discussed herein. Therefore, it is intended that this invention be limited only by the claims and the equivalents thereof.

Claims (13)

What is claimed is:
1. A detent device comprising:
a first hub having an axis and comprising a plurality of protruding ridges having both a radial and an axial dimension relative to the hub axis, and having a first hub connection portion; and
a second hub located co-axially outside the first hub and comprising a plurality of receiving grooves having both a radial and an axial dimension relative to the hub axis, the plurality of receiving grooves of the second hub touching the plurality of protruding ridges of the first hub when the plurality of protruding ridges and plurality of receiving grooves are aligned, the second hub having a second hub connection portion;
wherein the plurality of protruding ridges and plurality of receiving grooves have complementary mating geometries;
wherein the detent device is configured such that relative movement of the first and second hub connection portions causes a circumferential strain energy of the second hub to change, providing a variable force between the two connection portions depending on their relative position;
wherein a surface of the first hub defines a diameter and the plurality of protruding ridges extend from the surface a distance that does not exceed 4% of the diameter of the first hub; and
wherein the circumferential strain in the second hub causes at least 2% strain on the material of the second hub.
2. The detent device of claim 1, wherein one of the plurality of protruding ridges and plurality of receiving grooves causes bending strain energy on the second hub when the plurality of protruding ridges and plurality of receiving grooves are not aligned.
3. The detent device of claim 1, wherein one of the first and second hub comprises an engineered plastic and characterized in that the detent device is free of a lubricant between the first and second hubs.
4. The detent device of claim 1 configured to produce substantially consistent force as the first and second hub connection portions are rotated relative to each other for at least two thousand cycles of relative rotation.
5. The detent device of claim 1, wherein the first hub is rotationally grounded to an axis of a constant torque clutch.
6. A detent device comprising:
a first hub having at least two protruding ridges and a first hub connection portion; and
a second hub configured co-axially and adjacent the first hub and having at least two receiving grooves configured to receive and contact the respective two ridges of the first hub when the grooves and ridges are aligned, the second hub further configured with a second hub connection portion;
wherein relative movement of the first and second hub connection portions changes a circumferential strain energy of the second hub thereby providing a cyclical variable force between the first and second hub connection portions comprising a holding force when all ridges are within the grooves, followed by a maximum force when all ridges are moving out of the grooves, followed by a frictional force when all ridges are outside the grooves, followed by a negative force when all ridges are moving into the grooves, and wherein these forces repeat cyclically in sequence;
wherein a surface of the first hub defines a diameter and wherein the at least two protruding ridges extend from the surface a distance that does not exceed 4% of the diameter; and
wherein the circumferential strain in the second hub causes at least 2% strain on the material of the second hub.
7. The detent device of claim 6, wherein the first hub is co-axially within the second hub.
8. The detent device of claim 6, wherein the second hub is co-axially within the first hub.
9. The detent device of claim 6 further comprising the first hub having at least four protruding ridges and the second hub having at least four receiving grooves.
10. The detent device of claim 9, wherein the second hub is configured to expand circumferentially when the at least four ridges move out of the at least four receiving grooves and wherein the second hub is further configured to create a bending strain between two adjacent ridges when the at least four ridges are out of the at least four receiving grooves.
11. The detent device of claim 6, wherein one of the first and second hub comprises an engineered plastic and characterized in that the detent device is free of a lubricant between the first and second hubs.
12. The detent device of claim 6 configured to produce substantially consistent force as the first and second hub connection portions are rotated relative to each other for at least two thousand cycles of relative rotation.
13. A detent device comprising:
a first hub having an axis and comprising a plurality of grooves having both a radial and an axial dimension relative to the hub axis, and having a first hub connection portion; and
a second hub located co-axially outside the first hub and comprising a plurality of protruding ridges extending radially inward toward the first hub and having both a radial and an axial dimension relative to the hub axis, the plurality of protruding ridges of the second hub touching the plurality of grooves of the first hub when aligned, the second hub having a second hub connection portion;
wherein the plurality of grooves and plurality of protruding ridges have complementary mating geometries;
wherein the detent device is configured such that relative movement of the first and second hub connection portions causes a circumferential strain energy of the second hub to change, providing a variable force between the two connection portions depending on their relative position;
wherein an inner surface of the second hub defines an inner diameter and wherein the plurality of protruding ridges extend from the surface a distance that does not exceed 4% of the inner diameter; and
wherein the circumferential strain in the second hub causes at least 2% strain on the material of the second hub.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140215760A1 (en) * 2013-02-06 2014-08-07 Kason Industries, Inc. Lift-off type hinge
US9106016B1 (en) 2013-10-09 2015-08-11 Google Inc. Electrical connector
US9292049B1 (en) * 2013-07-19 2016-03-22 Google Inc. Variable torque hinge with pass-through cable
US10344512B2 (en) * 2016-12-07 2019-07-09 Elesa S.P.A. Hinge with defined halt positions
US20190321741A1 (en) * 2016-11-08 2019-10-24 Clicformers Nv Stackable hinge connection
US10463209B1 (en) 2018-04-17 2019-11-05 Kohler Co. Toilet seat hinge
US11269286B2 (en) * 2017-10-12 2022-03-08 Hewlett-Packard Development Company, L.P. Free stop based hinge apparatus

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2482143A1 (en) * 2011-01-26 2012-08-01 Nivarox-FAR S.A. Assembly by ratchet locking
CA2799868A1 (en) * 2011-12-29 2013-06-29 Taiwan Fu Hsing Industrial Co., Ltd. Transmission mechanism and electro-mechanical lock therewith
JP2014117039A (en) * 2012-12-07 2014-06-26 Nidec Copal Corp Geared motor
CN105468091B (en) * 2014-09-03 2019-01-15 联想(北京)有限公司 Electronic equipment and attachment device
EP3097886B1 (en) * 2015-05-29 2019-11-13 Greatbatch Ltd. Torque limiter having lobed shaped mechanism
CN109015751B (en) * 2018-07-12 2023-12-29 深圳市优必选科技有限公司 Robot and steering engine and overload protection structure thereof
CN114424078A (en) 2019-09-20 2022-04-29 皇家飞利浦有限公司 Damping mechanism, RF coil device and MRI apparatus
EP3832334A1 (en) * 2019-12-02 2021-06-09 Koninklijke Philips N.V. Damping mechanism, rf coil device and mri apparatus
US11596143B2 (en) * 2019-11-26 2023-03-07 Xtaris LLC Outdoor long-term storage enclosure
CN113494800A (en) * 2020-04-03 2021-10-12 博西华电器(江苏)有限公司 Refrigerator with a door
WO2023056080A1 (en) * 2021-10-01 2023-04-06 Music Express, Llc Hinge assembly

Citations (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458707A (en) 1946-02-23 1949-01-11 Jacobs Co F L Visor
US2572160A (en) 1945-04-09 1951-10-23 Gen Tire & Rubber Co Vibration absorbing bushing
US2572215A (en) 1945-04-09 1951-10-23 Gen Tire & Rubber Co Bushing and method of making same
GB747986A (en) 1954-03-27 1956-04-18 Autoyre Company Improvements in or relating to hinge connections in swinging arm racks
US3000049A (en) * 1958-08-04 1961-09-19 American Plastics Corp Plastic hinge and method of making the same
US3097150A (en) 1955-06-24 1963-07-09 Grace W R & Co Irradiated, cross-linked polyethylene copolymer
US3446340A (en) 1967-06-30 1969-05-27 William T Mullen Caulking strip
US3591674A (en) 1966-03-14 1971-07-06 Thomas Paul Engel Process for the preparation of polymeric materials
USRE29823E (en) 1974-05-13 1978-11-07 The General Tire & Rubber Co. Resilient bushing with long fatigue life
US4231135A (en) 1979-04-30 1980-11-04 Raymond Fradin Flexible and sewable hinge
US4445623A (en) 1982-09-30 1984-05-01 Kolling Byron M Molded trash container cover
US4452591A (en) 1980-08-26 1984-06-05 The Goodyear Tire & Rubber Company Resilient rotary coupling
US4506408A (en) * 1982-09-30 1985-03-26 Brown Dwight C Ratchet hinge structure
US4626112A (en) 1984-01-27 1986-12-02 The B.F. Goodrich Company Propeller bearing
US4654478A (en) 1978-03-02 1987-03-31 Ngk Insulators, Ltd. Electrical insulator including metal sleeve compressed onto a fiber reinforced plastic rod and method of assembling the same
US4667530A (en) 1985-07-22 1987-05-26 Etablissement Supervis Variable length shaft assembly particularly for motor vehicle steering shafts
US4688961A (en) 1985-03-15 1987-08-25 Nifco Inc. Combination clip
DE8621214U1 (en) 1986-08-07 1987-12-03 Lunke & Sohn Gmbh, 5810 Witten, De
US4734955A (en) * 1985-07-04 1988-04-05 Incoils Limited Hinge mechanism for a vehicle visor
US4861107A (en) 1988-06-13 1989-08-29 Hoover Universal, Inc. Head rest with forwardly pivotable pad mounted on friction hinge
US4927403A (en) 1987-02-24 1990-05-22 Pate Sr Kenneth D High voltage insulative shaft coupler
US4932924A (en) 1987-08-05 1990-06-12 Lohr & Bromkamp Gmbh Torque transmitting assembly
WO1990015265A1 (en) 1989-06-09 1990-12-13 Selsys Corporation Friction clutch mechanism
US5000721A (en) * 1987-08-20 1991-03-19 Itt Corporation Clutch apparatus
US5085289A (en) 1988-09-09 1992-02-04 Chance John H Shock-absorbing resilient coupling
JPH05248448A (en) * 1992-03-05 1993-09-24 Fuji Photo Film Co Ltd Torque limiter
US5253947A (en) 1990-10-23 1993-10-19 Gkn Automotive Ag Connection between a tubular shaft made of a fiber composite material and a metal journal, as well as a method of producing such a connection
US5397531A (en) 1992-06-02 1995-03-14 Advanced Materials Technologies Pte Limited Injection-moldable metal feedstock and method of forming metal injection-molded article
JPH0769075A (en) 1993-06-14 1995-03-14 Nishikawa Rubber Co Ltd Glass run channel for automobile
US5509176A (en) 1993-02-22 1996-04-23 Texas Instruments Incorporated Torque hinge
US5632071A (en) 1995-06-01 1997-05-27 Maunder; Martha Flexible hinge connector
US5765263A (en) * 1996-07-15 1998-06-16 Southco, Inc. Door positioning hinge
US5832566A (en) 1995-09-28 1998-11-10 Hewlett-Packard Company Friction hinge device
US5836821A (en) 1996-03-13 1998-11-17 Kabushiki Kaisha Yamada Seisakusho Elastic coupling for steering apparatus
US5924665A (en) 1996-06-07 1999-07-20 Ergotron, Inc. Ceiling system for a flat panel display
US5933917A (en) * 1998-01-06 1999-08-10 Delta Electronics Inc. Case with adjustable and positionable handle device
US6026776A (en) 1997-06-26 2000-02-22 Winberg; Randy S. Internal crankshaft vibration damper
US6085387A (en) 1998-05-18 2000-07-11 Phoenix Korea Co., Ltd. Hinge device
US6101676A (en) 1998-01-27 2000-08-15 Dell Usa, L.P. Adjustable clutch hinge assembly for portable computer
WO2000050717A2 (en) 1999-02-22 2000-08-31 ED. SCHARWäCHTER GMBH Motor vehicle door brake with holding function
US6173996B1 (en) 1997-11-25 2001-01-16 General Electric Company Compliant joint with a coupling member for interfacing dissimilar metals in X-ray tubes
US6230365B1 (en) 2000-01-11 2001-05-15 Lu Sheng-Nan Hinge for a notebook computer
US6281264B1 (en) 1995-01-20 2001-08-28 The Orthopaedic Hospital Chemically crosslinked ultrahigh molecular weight polyethylene for artificial human joints
US6286187B1 (en) 2000-03-03 2001-09-11 Jarlly Technology Co., Ltd. Rotary hinge shaft assembly
EP1160467A1 (en) 2000-05-30 2001-12-05 Nokia Corporation Turning mechanism for providing turning motion, and hinged electronic device
US20020174519A1 (en) 2001-05-23 2002-11-28 Kuo-Cheng Huang Hinge assembly for monitor
US6581267B1 (en) 1993-08-10 2003-06-24 Firma Carl Freudenberg Vibration canceler
EP1335090A1 (en) 2002-02-04 2003-08-13 ITW Fastex France Rotation-retarding device and use thereof
US6711781B2 (en) 2002-08-21 2004-03-30 Lite-On Technology Corporation Automatic releasing hinge
US6728993B1 (en) 2001-08-31 2004-05-04 Rikenkaki Kogyo Kabushiki Kaisha Structure for pivotally supporting check plate of door checker
US6871383B2 (en) 2002-09-17 2005-03-29 Hon Hai Precision Ind. Co., Ltd. Hinge device
WO2005027801A1 (en) 2003-09-18 2005-03-31 Smith & Nephew Inc. Prosthetic devices employing oxidized zirconium and other abrasion resistant surfaces contacting surfaces of cross-linked polyethylene
US6928700B2 (en) 2001-09-05 2005-08-16 Hing Basestrong Co., Ltd. Rotating shaft with radial press device
US7153571B2 (en) 2002-07-31 2006-12-26 Exxonmobil Chemical Patents Inc. Silane crosslinkable polyethylene
US20070212162A1 (en) 2006-03-08 2007-09-13 Scott Schank Shearing-force mechanism with cross-linked thermoplastic
US7377012B2 (en) 2005-05-27 2008-05-27 Hannspree, Inc. Axle positioning structure
US20090036609A1 (en) 2007-08-03 2009-02-05 Yuding Feng Rubber composition and vibration damper using the rubber composition
US20090038119A1 (en) 2007-08-07 2009-02-12 Edward Rude Friction hinge without applied grease
US7500288B2 (en) 2006-09-26 2009-03-10 Shin Zu Shing Co., Ltd. Hinge
US7578031B2 (en) 2008-06-02 2009-08-25 Protorsion Hinge Co., Ltd. Hinge structure with auxiliary roller unit
US7891055B1 (en) 2006-01-27 2011-02-22 Gary Combs Replacement hinge pin
US20110293356A1 (en) 2010-06-01 2011-12-01 Reell Precision Manufacturing Corporation Positioning and damper device using shear force from cyclic differential compressive strain of a cross-linked thermoplastic

Patent Citations (67)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572160A (en) 1945-04-09 1951-10-23 Gen Tire & Rubber Co Vibration absorbing bushing
US2572215A (en) 1945-04-09 1951-10-23 Gen Tire & Rubber Co Bushing and method of making same
US2458707A (en) 1946-02-23 1949-01-11 Jacobs Co F L Visor
GB747986A (en) 1954-03-27 1956-04-18 Autoyre Company Improvements in or relating to hinge connections in swinging arm racks
US3097150A (en) 1955-06-24 1963-07-09 Grace W R & Co Irradiated, cross-linked polyethylene copolymer
US3000049A (en) * 1958-08-04 1961-09-19 American Plastics Corp Plastic hinge and method of making the same
US3591674A (en) 1966-03-14 1971-07-06 Thomas Paul Engel Process for the preparation of polymeric materials
US3446340A (en) 1967-06-30 1969-05-27 William T Mullen Caulking strip
USRE29823E (en) 1974-05-13 1978-11-07 The General Tire & Rubber Co. Resilient bushing with long fatigue life
US4654478A (en) 1978-03-02 1987-03-31 Ngk Insulators, Ltd. Electrical insulator including metal sleeve compressed onto a fiber reinforced plastic rod and method of assembling the same
US4231135A (en) 1979-04-30 1980-11-04 Raymond Fradin Flexible and sewable hinge
US4452591A (en) 1980-08-26 1984-06-05 The Goodyear Tire & Rubber Company Resilient rotary coupling
US4445623A (en) 1982-09-30 1984-05-01 Kolling Byron M Molded trash container cover
US4506408A (en) * 1982-09-30 1985-03-26 Brown Dwight C Ratchet hinge structure
US4626112A (en) 1984-01-27 1986-12-02 The B.F. Goodrich Company Propeller bearing
US4688961A (en) 1985-03-15 1987-08-25 Nifco Inc. Combination clip
US4734955A (en) * 1985-07-04 1988-04-05 Incoils Limited Hinge mechanism for a vehicle visor
US4667530A (en) 1985-07-22 1987-05-26 Etablissement Supervis Variable length shaft assembly particularly for motor vehicle steering shafts
DE8621214U1 (en) 1986-08-07 1987-12-03 Lunke & Sohn Gmbh, 5810 Witten, De
EP0255879A2 (en) 1986-08-07 1988-02-17 Lunke & Sohn Aktiengesellschaft Vehicle door hinge with a door check
EP0255879B1 (en) * 1986-08-07 1991-09-04 Lunke & Sohn Aktiengesellschaft Vehicle door hinge with a door check
US4927403A (en) 1987-02-24 1990-05-22 Pate Sr Kenneth D High voltage insulative shaft coupler
US4932924A (en) 1987-08-05 1990-06-12 Lohr & Bromkamp Gmbh Torque transmitting assembly
US5000721A (en) * 1987-08-20 1991-03-19 Itt Corporation Clutch apparatus
US4861107A (en) 1988-06-13 1989-08-29 Hoover Universal, Inc. Head rest with forwardly pivotable pad mounted on friction hinge
US5085289A (en) 1988-09-09 1992-02-04 Chance John H Shock-absorbing resilient coupling
WO1990015265A1 (en) 1989-06-09 1990-12-13 Selsys Corporation Friction clutch mechanism
US5253947A (en) 1990-10-23 1993-10-19 Gkn Automotive Ag Connection between a tubular shaft made of a fiber composite material and a metal journal, as well as a method of producing such a connection
JPH05248448A (en) * 1992-03-05 1993-09-24 Fuji Photo Film Co Ltd Torque limiter
US5397531A (en) 1992-06-02 1995-03-14 Advanced Materials Technologies Pte Limited Injection-moldable metal feedstock and method of forming metal injection-molded article
US5509176A (en) 1993-02-22 1996-04-23 Texas Instruments Incorporated Torque hinge
JPH0769075A (en) 1993-06-14 1995-03-14 Nishikawa Rubber Co Ltd Glass run channel for automobile
US6581267B1 (en) 1993-08-10 2003-06-24 Firma Carl Freudenberg Vibration canceler
US6281264B1 (en) 1995-01-20 2001-08-28 The Orthopaedic Hospital Chemically crosslinked ultrahigh molecular weight polyethylene for artificial human joints
US5632071A (en) 1995-06-01 1997-05-27 Maunder; Martha Flexible hinge connector
US5832566A (en) 1995-09-28 1998-11-10 Hewlett-Packard Company Friction hinge device
US5836821A (en) 1996-03-13 1998-11-17 Kabushiki Kaisha Yamada Seisakusho Elastic coupling for steering apparatus
US5924665A (en) 1996-06-07 1999-07-20 Ergotron, Inc. Ceiling system for a flat panel display
US5765263A (en) * 1996-07-15 1998-06-16 Southco, Inc. Door positioning hinge
US6026776A (en) 1997-06-26 2000-02-22 Winberg; Randy S. Internal crankshaft vibration damper
US6173996B1 (en) 1997-11-25 2001-01-16 General Electric Company Compliant joint with a coupling member for interfacing dissimilar metals in X-ray tubes
US5933917A (en) * 1998-01-06 1999-08-10 Delta Electronics Inc. Case with adjustable and positionable handle device
US6101676A (en) 1998-01-27 2000-08-15 Dell Usa, L.P. Adjustable clutch hinge assembly for portable computer
US6085387A (en) 1998-05-18 2000-07-11 Phoenix Korea Co., Ltd. Hinge device
WO2000050717A2 (en) 1999-02-22 2000-08-31 ED. SCHARWäCHTER GMBH Motor vehicle door brake with holding function
US6230365B1 (en) 2000-01-11 2001-05-15 Lu Sheng-Nan Hinge for a notebook computer
US6286187B1 (en) 2000-03-03 2001-09-11 Jarlly Technology Co., Ltd. Rotary hinge shaft assembly
EP1160467A1 (en) 2000-05-30 2001-12-05 Nokia Corporation Turning mechanism for providing turning motion, and hinged electronic device
US6510588B2 (en) 2000-05-30 2003-01-28 Nokia Mobile Phones Ltd. Turning mechanism for providing turning motion, and hinged electronic device
US20020174519A1 (en) 2001-05-23 2002-11-28 Kuo-Cheng Huang Hinge assembly for monitor
US6728993B1 (en) 2001-08-31 2004-05-04 Rikenkaki Kogyo Kabushiki Kaisha Structure for pivotally supporting check plate of door checker
US6928700B2 (en) 2001-09-05 2005-08-16 Hing Basestrong Co., Ltd. Rotating shaft with radial press device
EP1335090A1 (en) 2002-02-04 2003-08-13 ITW Fastex France Rotation-retarding device and use thereof
US7153571B2 (en) 2002-07-31 2006-12-26 Exxonmobil Chemical Patents Inc. Silane crosslinkable polyethylene
US6711781B2 (en) 2002-08-21 2004-03-30 Lite-On Technology Corporation Automatic releasing hinge
US6871383B2 (en) 2002-09-17 2005-03-29 Hon Hai Precision Ind. Co., Ltd. Hinge device
WO2005027801A1 (en) 2003-09-18 2005-03-31 Smith & Nephew Inc. Prosthetic devices employing oxidized zirconium and other abrasion resistant surfaces contacting surfaces of cross-linked polyethylene
US7377012B2 (en) 2005-05-27 2008-05-27 Hannspree, Inc. Axle positioning structure
US7891055B1 (en) 2006-01-27 2011-02-22 Gary Combs Replacement hinge pin
US20070212162A1 (en) 2006-03-08 2007-09-13 Scott Schank Shearing-force mechanism with cross-linked thermoplastic
EP1999327A2 (en) 2006-03-08 2008-12-10 Reell Precision Manufacturing Corporation Shearing-force mechanism with cross-linked thermoplastic
US7500288B2 (en) 2006-09-26 2009-03-10 Shin Zu Shing Co., Ltd. Hinge
US20090036609A1 (en) 2007-08-03 2009-02-05 Yuding Feng Rubber composition and vibration damper using the rubber composition
US20090038119A1 (en) 2007-08-07 2009-02-12 Edward Rude Friction hinge without applied grease
US7578031B2 (en) 2008-06-02 2009-08-25 Protorsion Hinge Co., Ltd. Hinge structure with auxiliary roller unit
US20110293356A1 (en) 2010-06-01 2011-12-01 Reell Precision Manufacturing Corporation Positioning and damper device using shear force from cyclic differential compressive strain of a cross-linked thermoplastic
US8523476B2 (en) 2010-06-01 2013-09-03 Reell Precision Manufacturing Corporation Positioning and damper device using shear force from cyclic differential compressive strain of a cross-linked thermoplastic

Non-Patent Citations (30)

* Cited by examiner, † Cited by third party
Title
Advisory Action for U.S. Appl. No. 11/683,791 mailed Apr. 8, 2009 (3 pages).
Advisory Action for U.S. Appl. No. 12/791,834 mailed Nov. 6, 2012 (3 pages).
An English Translation of DE Office Action for Application No. 11 2011 101 885.1 mailed Feb. 26, 2014 (4 pages).
An English Translation of DE Office Action for Application No. 11 2011 101 885.1 mailed Oct. 17, 2013 (3 pages).
Applicant-Initiated Interview Summary for U.S. Appl. No. 12/791,834 mailed Jun. 26, 2012 (5 pages).
Applicant-Initiated Interview Summary for U.S. Appl. No. 12/791,834 mailed Oct. 10, 2012 (3 pages).
Decision on Appeal for U.S. Appl. No. 11/683,791 mailed Jul. 1, 2014 (8 pages).
E.I., du Pont de Nemours and Company, "Delrin(R)," DuPont Heritage: Delrin(R), pp. 1 (1995). .
E.I., du Pont de Nemours and Company, "Delrin(R)," DuPont Heritage: Delrin(R), pp. 1 (1995). <http://heritage.dupont.com/floater/fl—deirin/floater.shtml>.
Examiner's Answer for U.S. Appl. No. 11/683,791 mailed Jun. 17, 2011 (18 pages).
Final Office Action for U.S. Appl. No. 11/683,791 mailed Sep. 22, 2010 (17 pages).
Final Office Action for U.S. Appl. No. 111683,791 mailed Jan. 26, 2009 (9 pages).
Final Office Action for U.S. Appl. No. 12/791,834 mailed Aug. 23, 2012 (13 pages).
Final Office Action for U.S. Appl. No. 12/791,834 mailed May 2, 2012 (16 pages).
International Preliminary Report on Patentability for International Application No. PCT/US2007/005957 mailed Sep. 18, 2008 (8 pages).
International Preliminary Report on Patentability for International Application No. PCT/US2011/038178 mailed Dec. 13, 2012 (6 pages).
International Search Report and Written Opinion for International Application No. PCT/US2007/005957 mailed Aug. 31, 2007 (13 pages).
International Search Report and Written Opinion of the International Searching Authority for International Application No. PCT/US2011/038178 mailed Sep. 1, 2011 (11 pages).
International Search Report for International Application No. PCT/US2013/030517 mailed May 27, 2013 (5 pgs).
KLC, "Wirsbo AquapexTM, Engel Method Cross-Linked Polyethylene Technical Data Sheet," TECHPEX.doc, pp. 1 (May 4, 2005).
Notice of Allowance for U.S. Appl. No. 12/791,834 mailed Apr. 30, 2013 (11 pages).
Office Action for EP Application No. 07 752 641.6-2311 mailed Jul. 1, 2009 (3 pages).
Office Action for U.S. Appl. No. 11/683,791 mailed Aug. 7, 2008 (14 pages).
Office Action for U.S. Appl. No. 11/683,791 mailed Mar. 18, 2010 (10 pages).
Office Action for U.S. Appl. No. 12/791,834 mailed Jan. 13, 2012 (24 pages).
Wikimedia Foundation, Inc., "Delrin," Wikipedia, the free encyclopedia, pp. 1-3 (Jan. 18, 2007). .
Wikimedia Foundation, Inc., "PEX," Wikipedia, the free encyclopdia, pp. 1-3, (Feb. 2, 2007). .
Wikimedia Foundation, Inc., "Delrin," Wikipedia, the free encyclopedia, pp. 1-3 (Jan. 18, 2007). <http://en.wikipedia.org/wiki/Delrin>.
Wikimedia Foundation, Inc., "PEX," Wikipedia, the free encyclopdia, pp. 1-3, (Feb. 2, 2007). <http://en.wikipedia.org/wiki/PEX>.
Written Opinion of the International Searching Authority for International Application No. PCT/US2013/030517 mailed May 27, 2013 (6 pgs).

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140215760A1 (en) * 2013-02-06 2014-08-07 Kason Industries, Inc. Lift-off type hinge
US9416574B2 (en) * 2013-02-06 2016-08-16 Kason Industries, Inc. Lift-off type hinge
US9292049B1 (en) * 2013-07-19 2016-03-22 Google Inc. Variable torque hinge with pass-through cable
US9106016B1 (en) 2013-10-09 2015-08-11 Google Inc. Electrical connector
US20190321741A1 (en) * 2016-11-08 2019-10-24 Clicformers Nv Stackable hinge connection
US10344512B2 (en) * 2016-12-07 2019-07-09 Elesa S.P.A. Hinge with defined halt positions
US11269286B2 (en) * 2017-10-12 2022-03-08 Hewlett-Packard Development Company, L.P. Free stop based hinge apparatus
US10463209B1 (en) 2018-04-17 2019-11-05 Kohler Co. Toilet seat hinge

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